Chinese
您当前的位置：
首页 >
文章列表页 >
常规推进剂火箭发动机膜冷却长度试验与仿真
更新时间：2025-03-14

    • 常规推进剂火箭发动机膜冷却长度试验与仿真

    • Vol. 38, Issue 11, Pages: 2799-2808(2023)

    • DOI：10.13224/j.cnki.jasp.20230038    

      CLC：

    移动端阅览

  • 侯瑞峰, 陈建华, 李龙飞, et al. 常规推进剂火箭发动机膜冷却长度试验与仿真[J]. 2023, 38(11): 2799-2808. DOI： 10.13224/j.cnki.jasp.20230038.

  •  
  •  
icon
试读结束，您可以激活您的VIP账号继续阅读。
去激活 >
icon
试读结束，您可以通过登录账户，到个人中心，购买VIP会员阅读全文。
已是VIP会员？
去登录 >

0

Views

117

下载量

0

CSCD

Alert me when the article has been cited
提交
Tools
Download
Export Citation
Share
Add to favorites
Add to my album

Related Articles

液体火箭发动机不同室压下冷却方案适用范围
流场不均匀对液体火箭发动机纵向振荡燃烧影响及控制
General simulation on modularization of liquid rocket engine
Analysis of thermo-structure for attitude liquid rocket engine in ground test
Reliability compliance test plans for liquid-propellant rocket engine based on weighting factors

Related Author

李龙飞
曹晨
刘云浩
李龙飞
杨宝庆
葛树宏
刘佩进
刘新华

Related Institution

西北工业大学航天学院
School of Astronautics, Beijing University of Aeronautics and Astronautics
School of Astronautics, Northwestern Polytechnical University,Xian
Beijing Institute of Astronautical Systems Engineering, China Academy of Launch Vehicle Technology
School of Reliability and Systems Engineering, Beijing University of Aeronautics and Astronautics
0